About 19 results
https://drivepatents.com/patents/1388500 · 10 Jun 2026
An assembly (200) for mounting an auxiliary component to an engine case (110) of a gas turbine engine (100) includes a support bracket (122), the support bracket having a first end (230) configured for attachment to a first flange (232) of the engine case,...
https://drivepatents.com/patents/1387145 · 13 May 2026
A blade containment assembly for a gas turbine engine (10) comprises a casing (15) having a first casing member (15a) surrounding a set of rotor blades (14c) and a second casing member (15b) extending axially from the first casing member (15a). The first c...
https://drivepatents.com/patents/1393659 · 8 Oct 2025
A gas turbine engine (20) is provided and includes a first fan blade including a suction surface, a second fan blade comprising a pressure surface and neighboring the first fan blade and a throat region interposed between the suction surface of the first f...
https://drivepatents.com/patents/969315 · 1 Oct 2014
A rigid electrical raft (200) is provided to a gas turbine engine via a fusible mount arrangement (400). The rigid electrical raft may be a part of an electrical system of the gas turbine engine, for example a part of the electrical harness. The fusible mo...
https://drivepatents.com/patents/971098 · 20 Aug 2014
A fan containment system (200) arranged to be fitted around an array of radially extending fan blades (40) mounted on a hub in an axial gas turbine engine. The fan containment system comprises: a generally cylindrical fan case (250) including a hook (260) ...
https://drivepatents.com/patents/971038 · 20 Aug 2014
This invention relates to the operation of gas turbine engines (10), and in particular to determining deterioration of components during operation. In a specific embodiment, the invention is concerned with determining the actions to be taken when a foreign...
https://drivepatents.com/patents/989535 · 19 Jun 2013
A fan case (72) of a gas turbine engine includes a fan blade containment section (78) defined about an engine axis (A) and a plurality of helical ribs (92) adjacent to the fan blade containment section (78). The plurality of helical ribs are within a thrus...
https://drivepatents.com/patents/997019 · 24 Oct 2012
A gas turbine engine (10) comprises a nacelle assembly (25), a core engine (25) at least partially surrounded by the nacelle assembly (35) and including a fan section (14), a compressor section (16), a combustor section (22) and a turbine section (24) and ...
https://drivepatents.com/patents/998576 · 5 Sep 2012
A turbomachine casing assembly 100;200;300 comprises a first casing element 110;210;310 locatable radially outward of one or more rotating aerofoil elements 130 of a turbomachine, a second casing element 120 located radially distal to the first casing elem...
https://drivepatents.com/patents/1003897 · 28 Mar 2012
A disclosed fan containment case (26) includes a fan case fabricated from a plurality of non-metallic composite layers (38) with an attachment flange formed of both a composite portion (32) and a metallic backing (42). The disclosed metallic backing (42) i...